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最优非线性控制技术在导弹控制中的研究与应用
引用本文:孙赵根.最优非线性控制技术在导弹控制中的研究与应用[J].航天控制,2005,23(1):41-44.
作者姓名:孙赵根
作者单位:北京航天自动控制研究所,北京,100854
摘    要:首先运用相平面分析方法,推导了相轨迹运动方程,分析了传统控制方 法影响控制精度的主要因素和解决途径;然后运用最优控制理论,结合实际特 性,采用二次型开关线设计控制规律,对时间短和燃料省的混合指标最优控制问 题进行了探讨。仿真结果表明,该设计方法简单、可靠,具有工程实用价值。

关 键 词:非线性控制系统  极限环  最优控制  仿真
文章编号:1006-3242(2005)01-0041-04
修稿时间:2004年9月6日

Research and Application of Optimal Nonlinear Control Theory in Missile Control
Sun Zhaogen.Research and Application of Optimal Nonlinear Control Theory in Missile Control[J].Aerospace Control,2005,23(1):41-44.
Authors:Sun Zhaogen
Institution:Sun Zhaogen Beijing Aerospace Automatic Control Institute,Beijing 100854
Abstract:In this paper, the phase path motion equation is derived by using phase plane method firstly. In the traditional control methods the primary factors which effects control precision are analyzed and its solutions are proposed. Furthermore, according to the practice characteristics, the control law is designed by using the quadratic switch line method and optimal control theory. The optimal control problem with complex index combining shorter time and fewer fuel is also discussed. Simulation results show that the designed method possesses advantages such as simplicity, reliability and good perspective of engineering application.
Keywords:Nonlinear control system  Limit circle  Optimal control  Simulation  
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